LEADER 01216nam a2200265 i 4500 001 991003349969707536 008 080218s2005 it |||||||||||||||||ita d 020 $a9788823830899 035 $ab13673749-39ule_inst 040 $aISUFI - Sett. Patrimonio Culturale$bita 082 04$a346.4506648 245 00$aBilancio e reddito d'impresa :$baggiornato al correttivo IRES : disciplina civilistica e fiscale, analisi di bilancio /$cGiovanni M. Conti ... [et al.] ; presentazione di Arturo Sanguinetti 260 $aMilano :$bEGEA,$c2005 300 $axx, 1162 p. :$bill. ;$c24 cm 440 0$aLa riforma delle società 650 0 $aBilancio$xLegislazione 650 0 $aImprese$xRedditi$xTributi$xLegislazione 700 1 $aConti, Giovanni Maria 907 $a.b13673749$b02-04-14$c18-02-08 912 $a991003349969707536 945 $aLE016 346.4506648 CON 01.01$g1$i2016000081763$lle016$on$pE80.00$q-$rn$so $t0$u0$v0$w0$x0$y.i1472926x$z17-04-08 945 $aLE025 ECO 346 CON01.02$g1$i2025000107014$lle025$n2010$o-$pE80.00$q-$rl$s- $t0$u0$v0$w0$x0$y.i15104886$z07-04-10 996 $aBilancio e reddito d'impresa$91057772 997 $aUNISALENTO 998 $a(2)le016$ale025$b18-02-08$cm$da $e-$fita$git $h0$i0 LEADER 01914oam 2200541 450 001 9910717297703321 005 20220225133249.0 035 $a(CKB)5470000002529245 035 $a(OCoLC)1158388771 035 $a(EXLCZ)995470000002529245 100 $a20200615d1941 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 14$aThe compressive yield strength of extruded shapes of 24ST aluminum alloy /$fby R.L. Templin, F.M. Howell, and E.C. Hartmann 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1941. 215 $a1 online resource (11 pages, 7 unnumbered pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vno. 793 300 $a"January 1941." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 8). 606 $aAluminum alloys 606 $aMaterials$xCompression testing 606 $aStrength of materials 606 $aAluminum alloys$2fast 606 $aMaterials$xCompression testing$2fast 606 $aStrength of materials$2fast 615 0$aAluminum alloys. 615 0$aMaterials$xCompression testing. 615 0$aStrength of materials. 615 7$aAluminum alloys. 615 7$aMaterials$xCompression testing. 615 7$aStrength of materials. 700 $aTemplin$b R. L.$01423297 702 $aHowell$b F. M. 702 $aHartmann$b E. C. 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910717297703321 996 $aThe compressive yield strength of extruded shapes of 24ST aluminum alloy$93550453 997 $aUNINA